Apparatus for the destruction of volatile organic compounds

ABSTRACT

A system for the destruction of volatile organic compounds while generating power. In a preferred embodiment the system comprises a combustor and a reaction chamber connected to an exit of the combustor. A primary inlet to the combustor supplies a primary fuel to the combustor. A secondary fuel, comprising air and an amount of one or more volatile organic compounds, is supplied to a compressor, which compresses the secondary fuel and directs the secondary fuel to the combustor and the reaction chamber. The system is suitably configured to enable the stoichiometric reaction of the two fuels in a manner sufficient to destroy the volatile organic compounds contained in the secondary fuel and power a turbine engine connected to an exit of the reaction chamber.

TECHNICAL FIELD

This invention relates generally to a method and apparatus for thedestruction of hazardous materials, such as volatile organic compounds,and more particularly, to the destruction of volatile organic compoundsthrough the use of a turbine engine in order to produce power.

BACKGROUND OF THE INVENTION

Increasingly over the past half century, air quality has become an issueof public concern. Over this period, the scientific community hassteadily improved its understanding of the origins of the air pollutionthat is apparent over most major U.S. cities. A large part of this airpollution is attributable to the release of volatile organic compoundsinto the atmosphere. As a result, the reduction of the releases ofvolatile organic compounds has become an increasingly important part ofthe overall strategy to improve air quality.

The most familiar volatile compound reduction technique is the controlof fuel vaporization by vapor recovery techniques, first on automobilesand now on gasoline stations located in nonobtainment areas. As aresult, the steady year over year increase in U.S. releases of thesecompounds has leveled off and is now even declining.

Manufacturing sites are responsible for approximately 8.5 million tonsof volatile organic compound emissions annually. Solvent vaporization orin some cases, hydrocarbon byproducts, are key to the manufacturingprocess of many of the items used regularly in daily life. Themanufacture of familiar consumer products results in the release intothe atmosphere of significant amounts of organic compounds such aspentane, ethanol, methanol, ethyl acetate, and many others. The controlof volatile organic compounds is essential to the environmentallyfriendly manufacture of these products, and thus, there remains astruggle with the cost of control versus the loss of competitiveness.

The most common control method in use today is the thermal oxidizer. Inconnection with this method, the volatile solvent is released in amountsgenerally less than a few thousand parts per million into the plant airsystem. This air is then selectively collected and fed into a combustionchamber where it is mixed with enough natural gas to sustain combustion.It is then ignited in a large chamber that incinerates the volatilesolvent, as well as, the natural gas, thereby producing carbon dioxideand water vapor as the primary products of combustion. These oxidizersare large, complicated devices that represent a major capital expenseand require significant amounts of electricity and gas to operate. Whileheat can sometimes be recovered, generally speaking, thermal oxidizersrepresent a significant economic loss to the businesses using them. In atypical U.S. industrial plant, the cost of operating this type of deviceeasily adds 25%, and often much more, to the yearly energy bill.

Another current control technology uses solvent recovery methods thatpass the air from the plant through an activated charcoal filter.Periodically, the charcoal is heated, driving off highly concentratedvolatile compounds into a chilled condensing system. The output is aliquid organic compound often requiring hazardous waste treatment. Thecost of operation, as well as the initial capital costs, aresignificantly higher than the thermal oxidizer, thereby making thiscontrol technology less attractive for the majority of industrial sites.

Accordingly, an efficient and cost effective device for the destructionof volatile organic compounds is needed.

Such a device is described and claimed in the copending application U.S.Ser. No. 08/538,692, now U.S. Pat No. 5,592,811, filed on Oct. 3, 1995,and owned by the assignee of record. The subject matter of thatapplication is hereby incorporated herein by reference.

In that application, a system for the destruction of volatile organiccompounds is disclosed which comprises a combustor and a reactionchamber, both of which are suitably connected to the compressor, such asthe compressor of a power generator (e.g. a gas turbine engine). Thesystem further comprises a primary inlet to the combustor for supplyinga primary fuel and a secondary inlet to the combustor and the reactionchamber for supplying a secondary fuel. The secondary fuel comprises airand an amount of a volatile organic compound. The compressor compressesthe secondary fuel and directs the compressed fuel to the combustor andreaction chamber. The fuel mixture is reacted in the reaction chamber,and the stream of combustion gases directed to a power generator togenerate power.

While the system so described is suitable for use in many applications,once assembled, particularly if the combustor is provided for direct, inline communication with the inlet of the reaction chamber, the size ofthe device becomes cumbersome for shipping and maintenance.

Moreover, in operation of the device, particularly when the VOC ladenair is drawn from environments which vary over time, i.e. the amount ofVOCs in the air varies, control of the system can become difficult.

SUMMARY OF THE INVENTION

A system for the destruction of volatile organic compounds according tothe present invention addresses the shortcomings of the prior art,particularly those difficulties which may be encountered during use of asystem in accordance with some aspects of the system described in theaforementioned copending application.

In accordance with one aspect of the present invention, a system for thedestruction of volatile organic compounds comprises a power generator, acompressor, a combustor and a reaction chamber. A primary inlet to thecombustor is provided for supplying a primary fuel to the combustor. Asecondary fuel comprising air and at least one volatile organic compoundis provided to the compressor. An outlet from the compressorcommunicates with the reaction chamber and the combustor. The combustoris attached to the reaction chamber such that the flow of combustedgasses is directed tangentially into the reaction chamber, therebyenhancing the residence time of the mixed fuels within the reactionchamber. In addition, the size of the device is suitable for shipping. Apower generator is connected to an exit of the reaction chamber andutilizes the exiting fuel mixture to generate power.

In accordance with a further aspect of the present invention, thecombustor and the reaction chamber are configured to create a cyclonicflow of the primary and secondary fuels through the reaction chamber.This allows for the fuel to remain in the reaction chamber for a longerperiod of time, thereby providing for a better stoichiometric reaction.

In accordance with a further aspect of the present invention, an airflow system is provided to regulate the inlet air and fuel supplieswithin the combustor and reaction chamber to maintain effectiveoperation of the device.

BRIEF DESCRIPTION OF THE DRAWING FIGURES

The present invention will hereinafter be described in conjunction withthe appended drawing figures, wherein like designations denote likeelements, and:

FIG. 1 is a simplified schematic drawing of a destruction device inaccordance with the present invention;

FIG. 2 is a schematic drawing of a device of the type shown in FIG. 1 asutilized in an exemplary plant layout;

FIG. 3 is a cross-sectional view of a combustor used in connection withthe destruction device of FIG. 2;

FIG. 4 is a partial cross-sectional view of the combustion device andreaction chamber of the destruction device of FIG. 2;

FIG. 5 is a cross-sectional view of the compressor of the destructiondevice of FIG. 2;

FIG. 6 is a schematic drawing of an alternative plant layout of adestruction device in accordance with the present invention; and

FIG. 7 is a further alternative embodiment of a mobile layout of adestruction device in accordance with the present invention.

DETAILED DESCRIPTION OF PREFERRED EXEMPLARY EMBODIMENTS

While the way in which the present invention addresses the variousdisadvantages of the prior art designs will be discussed in greaterdetail hereinbelow, in general, the present invention provides avolatile organic compound (VOC) destruction device which includes apower generator such that the effective elimination of VOC's alsoresults in the co-generation of power. The power so produced can beconverted into electricity, which can in part drive the destructiondevice as well as produce power for other uses.

With reference to FIGS. 1 and 2, a VOC destruction device 10, inaccordance with a preferred embodiment of the present invention,suitably includes a power generator 12 which is driven by a fuel system14. Fuel system 14 preferably comprises a combustor 16 and a reactionchamber 18. As will be discussed in greater detail hereinbelow, inoperation, VOC destruction device 10 utilizes natural gas or any othersuitable fuel as a primary fuel supply in a conventional manner.However, in accordance with the present invention, this primary fuel issuitably mixed with a secondary fuel comprising air and preferably VOCs.This fuel mixture of primary and secondary fuels is burned in powergenerator 12.

In accordance with a preferred embodiment of the present invention,power generator 12 preferably comprises a gas turbine engine, forexample an AlliedSignal IE-831 engine, which is produced by AlliedSignalAerospace, Phoenix, Ariz. has been found to be suitable. However, itshould be recognized that any suitable engine can be used in the contextof device 10, provided such engine can be suitably employed in thegeneration of power.

With continued reference to FIG. 2, power generator (engine) 12 ispreferably of a conventional design. For example, engine 12 suitablyincludes, in spaced relation, a generator 20, a gearbox 22, a compressor24 and a turbine 26. Turbine 26, also preferably of a conventionaldesign, suitably includes a power turbine (not shown) connected to shaft28. As will be appreciated, shaft 28 is suitably connected to generator20, gearbox 22 and compressor 24.

In accordance with the present invention, VOC destruction device 10 canbe utilized to concurrently destroy VOC's and realize the fuel value ofsuch VOC's produced from a variety of different environments. In thiscontext, the term "VOC" is used broadly to refer to carbon containingcompounds, such as hydrocarbons, dioxins, alcohols, ketines aldehydes,ethers, organic acids, halogenated forms of the foregoing and the like.For example, as used herein, the term VOC may refer to pentane,n-ethylmorphilin, toluene, ethanol, methanol, decabromodiphenyloxide,ethyl acetate, benzene, polystyrene and the like. Such VOC's or similarchemical compounds are typically produced from the evaporation ofchemicals used in and generated by basic industrial processes to produceplastics, pharmaceuticals, bakery products, printed products and thelike. A particularly preferred application of the present invention isin the area of control VOC's produced during the production ofexpandable polystyrene (i.e. the process to make "styrofoam") where theprimary emission is the VOC pentane.

Device 10 can be employed to destroy VOC's which can be collected fromthe plant as whole, from special isolated or hooded areas, from dryersor from a VOC concentrator utilized in such plants. In the context ofthe present invention, air from one or more of these environments orareas is referred to as "VOC laden air". It should be appreciated thatthe amount of VOC present in such air may vary from small amounts ornone to larger amounts, over time and as conditions in the plant change.As with typical prior art methods of destroying VOCs or such, thepresent invention may be employed even over periods of time when the VOClevel is small or nonexistent. As such, the term VOC laden air includesair that from time to time may not include a significant quantity (orany amount) of a VOC.

VOC laden air, such as air laden with pentane resulting from themanufacture of expandable polystyrene, is first collected and thereaftersuitably passed into device 10. While such VOC laden air may becollected in any conventional manner for use in connection with thepresent invention, preferably, in such a process, the VOC laden air isducted from the plant via one or more air ducts. These ducts aredirectly or indirectly connected to an inlet duct 40 (see FIG. 1) whichprovides VOC laden air to destruction device 10.

In accordance with a preferred aspect of the present invention, powergenerator 12 draws in such VOC laden air together with fuel, thecombustion gases of both Which flow at high velocity into turbine 26 andthereby drive turbine 26. As previously briefly mentioned, the primaryfuel utilized in accordance with the present invention may comprisenatural gas; alternatively, diesel oil, jet fuel, methane or any otherfuel material may be utilized in an amount sufficient to sustaincombustion in combustor 16.

The secondary fuel comprising the VOC laden air is generally much leanerthan the primary fuel. Generally speaking, the secondary fuel has a VOCconcentration in the range of 0% to 1%. This 1% maximum corresponds toapproximately 10,000 parts per million, depending on the type of organiccompound involved. Typically this will comply with OSHA regulations asthe maximum concentration allowed within plant air in order to preventthe possibility of an explosion within the plant, and in the eventpermissible limits are exceeded, the concentration can be reduced.However, it should be appreciated that system 10 is capable of handlinghigher VOC concentrations, as may be desirable in some applications.

With reference to FIG. 1, a simplified schematic view of destructiondevice 10 is shown. As shown, VOC laden air from inlet duct 40 issuitably directed to power generator 12, and in particular, compressor24 thereof. Preferably, the temperature of the inlet air A, i.e. the VOCladen air, is at a temperature of less than about 130° F. To this end, atemperature control system 42 is suitably positioned to measure thetemperature of the inlet air and in the event the temperature exceedsabout 130° F., the air is cooled through a cooling system 44. As will beappreciated by those skilled in the art, cooling system 44 may suitablycomprise an air or water heat exchanger suitably configured to cool thetemperature of inlet air to a temperature in the range of about 59° toabout 130° F.

Once the temperature of inlet air A is within a suitable range, suchinlet air A is passed through a control valve 46 which is suitablyprovided with a VOC monitor 48. As will be discussed in greater detailbelow, monitor 48 measures the level of VOC within inlet air A. This VOClevel measurement, as will be described in greater detail below, isutilized to adjust, as appropriate, the ratio of primary and secondaryfuels which are fed into combustor 16. Regulator 46 suitably regulatesthe flow of air which is drawn into compressor 24.

When device 10 is placed in initial operation, generator 20 is utilizedto initially drive compressor 24 (as well as turbine 26) to suitablydraw inlet air A into compressor 24. As operation of device 10continues, the power drawn from generator 20, through gearbox 22, may besuitably decreased and thereafter compressor 24 is, at least in part,and preferably entirely driven by the power generated through operationof device 10, and in particular, through the generation of energyeffected by turbine 26.

As discussed briefly above, compressor 24 suitably comprises thecompressor of power generator 12. With momentary reference to FIG. 5,compressor 24 preferably comprises alternate respective sets of rotatingblades 56 and stationary blades 58. Rotating blades 56 are suitablyrotated through rotation of shaft 28, which is briefly noted above, isinitially activated by generator 20. In accordance with a preferredaspect of the present invention, compressor 24 comprises a multistagecompressor, more preferably a two stage compressor, i.e. there are atleast 2 rotating blades (impellers) 56 within the body of compressor 24.

As will be recognized by those skilled in the art, inlet air A drawninto compressor 24 is suitably compressed to pressures ranges from about4 to about 30 atmospheres, and preferably to about 9 atmosphere. Thiscompression raises the temperature of inlet air A, and thus thesecondary fuel, to ideally about 600° F., but suitably within the rangeof about 550° F. to about 650° F. The compressed air B then exitscompressor 24 through outlets 57A, 57B and preferably enters reactionchamber 18 through inlets 59A, 59B.

With continued reference to FIG. 1, compressed air B is suitablydirected to a flow valve 50 which is provided with a monitor 52. Valve50 suitably controls the amount of compressed air B which is provided toreaction chamber 18 and combustor 16.

As shown best in FIG. 1, a primary fuel inlet 70 provides primary fuel Cto combustor 16 through a flow valve 72. Flow valve 72 preferablyincludes a monitor 74 to monitor the volume of fuel which is provided tocombustor 16. As will be described in greater detail hereinbelow, fuel Cand a limited amount of compressed air B (including the secondary VOCfuel) is suitably provided to combustor 16, the remaining portion of thesecondary fuel being provided to reaction chamber 18. In accordance witha particularly preferred aspect of the present invention, thecombination of combustor 16 and reaction chamber 18 is effective tosubstantially destroy the VOC within compressed air B and provide amixed combustion gas stream D having a temperature suitable to activatethe nozzle and turbine stages of gas turbine 26. In accordance with apreferred aspect of the present invention, the mixed-out temperature ofmixed stream D provided to turbine 26 is in the range between about1500° F. and about 2300° F., preferably about 1850° F.

In a conventional fashion, mixed stream D is directed to turbine 26.Turbine 26 of the type generally described above, is initially startedby cranking it over with a starter (not shown) to produce air flowthrough the compressor. At the appropriate speed, fuel C is permitted toflow into combustor 16. However, once device 10 is in operation, mixedstream D suitably powers turbine 26 in a manner such that the output Efrom turbine 26 is suitably harnessed and utilized in subsequentoperation of device 10, as well as in connection with the production ofpower for other applications.

With reference to FIGS. 3 and 4, the way in which reaction chamber 18and combustor 16 cooperatively work to effectively destroy the VOC's inthe VOC laden air in a manner to suitably drive power generator 12 willnow be described in greater detail.

Reaction chamber 18 preferably comprises a double walled vessel having amain, inner wall 60 and an outer wall 62 that envelopes inner wall 60.The chamber 64 defined by walls 60 and 62 is suitably configured andpositioned in proximity to compressor 24 to receive compressed air B.Preferably, and with reference to FIGS. 4 and 5, chamber 64 receivescompressed air B (containing the secondary fuel) from outlets 57A, 57Bof compressor 24. Chamber 64 extends about the periphery of reactionchamber 18. Further, in accordance with a preferred aspect of thepresent invention, chamber 64 also suitably communicates with combustor16 in the region of respective openings 67A and 67B by way of aplurality of inlets 69, as well as by way of tube outlets 124, 126.Thus, compressed air B is, in accordance with at least one aspect of thepresent invention, suitably provided to the combustor 16 and alsodirectly to chamber 64 by way of tubes 116, 118, as will be discussed infurther detail below.

With reference to FIG. 3, combustor 16 preferably comprises a hot walltype thermally insulated combustor. Preferably, combustor 16 comprisesan outlet wall 80 within which a conventional combustion device 82 issuitably orientated. An inlet 84 communicates with combustion device 82to advantageously effect combustion of fuel C. As previously brieflymentioned, fuel inlet C is preferably directed from fuel supply 70through fuel control valve 74 and compressed air B is provided tocombustion device 82 through inlets 69. In accordance with preferredaspects of the present invention, fuel supply C is suitably controlledby a control system 150 such that a sufficient amount of primary fuel Cis provided to the combustion chamber to effectively maintain anappropriate equivalence ratio (ER) thereby enabling stoichiometricallycorrect combustion. As shown best in FIGS. 3 and 4, the outlet 86 ofcombustor 16 suitably communicates with the interior of reaction chamber18.

Combustor 16 may be attached to reaction chamber 18 in any convenientmanner. For example, combustor 16 can be fixably attached to chamber 18such that outlet 86 of combustor 16 directly communicates with anopening of reaction chamber 18 in an in-line manner. However, inaccordance with a preferred aspect of the present invention and as shownbest in FIGS. 3 and 4, combustor 16 is attached to reaction chamber 18such that combustor 16 is orthogonal to the central axis X of reactionchamber 18. In this manner, as will be described in greater detailbelow, the combustion gases exit outlet 86 of combustor 16 tangentiallyto reaction chamber 18 thereby tending to create a substantiallycyclonic flow of the resulting fuel mixture within reaction chamber 18.While combustor 16 is shown in FIG. 4 as being attached to reactionchamber 18 tangentially near an end of reaction chamber 18 oppositeinlets 59a, 59b, it should be appreciated that combustion chamber 16 maybe attached in any convenient fashion. For example, combustor 16 may beattached at any angle from about 0 to about 90° from the central axis Xof reaction chamber 18 and at any point along a side or the top ofreaction chamber 18.

Combustion within combustor 16 takes place in a generally conventionalmanner, with the exception that compressed air B, i.e. the VOC laden airintroduced into the system, is permitted to mix with the primary fuel Cwithin the later stages of combustor 16. As will be appreciated by thoseskilled in the art, near inlet 84, primary fuel C is relatively richsuch that it burns under near stoichiometric conditions, typically at atemperature in the range of about 2500° F. to about 3200° F., preferablybetween about 2800° F. and about 3000° F. and optimally 3000° F. In thisregion denoted in FIGS. 3 and 4 as "P", often referred to as the"primary zone", a minor portion of secondary fuel B is suitably mixedwith primary fuel thereby creating a fuel mixture of primary andsecondary fuels. The minor portion of secondary fuel introduced into theprimary-zone P is about 10% to about 30% of the secondary fuel. If theportion falls much below 10%, the fuel will become too rich and therebycause "rich blowout." While the amount of secondary fuel introduced intocombustor 16 will vary, in general preferably from about 0 to about 70%,and more preferably from about 0 to about 50% of the fuel necessary todrive power generator 12 is provided by the secondary fuel.

The residence time of the gas mixture of primary fuel and secondary fuelwithin reaction chamber 18 is enhanced due to the preferredconfiguration of combustor 16 relative to reaction chamber 18.Specifically, and in accordance with a preferred aspect of the presentinvention, as the combustion gases exit the combustor at outlet 86, suchgases are directed toward the opposing wall of reaction chamber 18. Theflow pattern which results in the interior of reaction chamber 18 tendsto be cyclonic, i.e. creating a spiral pattern.

In accordance with a preferred aspect of the present invention, the fuelmixture, comprising primary fuel and secondary fuel is retained inreaction chamber 18 for a sufficient time to effectively burn, i.e.combust the VOC's contained within the secondary fuel B. Typically, theresidence time of the gas mixtures within reaction chamber 18 is on theorder of about 0.25 seconds or more. In accordance with a preferreddesign of the present invention, the tangential orientation of thecombustor relative the reaction chamber has been found to not onlyenhance residence time, but also to cause a degree of recirculationwithin reaction chamber 18 thus further enabling substantially completedestruction of the VOC's within reaction chamber 18.

In practice, the present invention generally results in an excess of90%, and typically from between about 95 and 99.5% of the VOC containedwithin secondary fuel B being effectively broken down into water vaporand carbon dioxide. As will be appreciated, and as will be discussed ingreater detail below, through effective operation of device 10,substantially all of the VOCs contained within the inlet air A, and thuscompressed air B, are thus effectively destroyed within reaction chamber18 and/or combustor 16.

The double-walled configuration of reaction chamber 18, which permitsflow of compressed air B through the outer chamber 64 advantageouslyprovides for a modicum of cooling of the reaction chamber. For example,in the region of the outlet 90 of reaction chamber 18 cooling tends totake place due to the generally lower temperature of the compressed airB as compared to the temperature of the combusting fuel mixture withinthe inner portion chamber of reaction chamber 18.

Outlet 90 of chamber 18 suitably communicates with turbine 26 of powergenerator 12. In a conventional fashion, the high velocity flows of thecombusted gas mixture flow onto turbine 26 to thereby drive it. Turbine26 is suitably configured, in a conventional fashion, to produce usablepower to not only continue operation of device 10, but also to providepower for other applications. For example, through utilization of apreferred gas turbine engine, e.g. an AlliedSignal IE-831 engine, inconnection with destruction device 10 of the present invention, powersufficient to run compressor 24 and up to an additional 525 kw ofelectricity have been found to be obtainable.

With reference to FIG. 2, in accordance with a preferred embodiment ofthe present invention, power generator 12 is suitably positioned suchthat the exhaust heat E is directed to a heat recovery system 100. Heatrecovery system 100 may be of conventional design and operate in aconventional fashion. For example, system 100 may comprise a heatrecovery steam generator suitably configured and positioned to provideusable hot water 102 and steam 104. As also shown in FIG. 2, water 102can be converted into power sufficient to power gearbox 22, therebyobviating the continuing need for generator 20, and steam 104 can bereleased as process heat or recirculated into the regional combustor 16.

Alternatively, exhaust E may be directly used. Exhaust E is generally ata temperature of about 1000° F., and thus can be used to heat the plantdirectly. Because as much as about 99.5% or more of the VOCs have beeneffectively destroyed through operation of device 10, exhaust E can bereleased directly into the atmosphere.

In accordance with a further aspect of a preferred exemplary embodimentof the present invention, device 10 is suitably provided with an inletair control system 110. With reference to FIG. 4, system 110 mayadvantageously comprise a bypass flow circuit comprising respectivebypass flow channels 112, 114.

As will be appreciated by those skilled in the art, combustor 16requires a certain primary-zone fuel-to-air ratio to operate properly,typically 0.04 to 0.05, while power generator 12 typically requires afuel-to-air ratio of approximately 0.008-0.01. Accordingly, the fuelratio within combustor 16 generally should be richer than, e.g. aboutfour to five times as rich as, the overall fuel ratio required by thegenerator 12 at idle or with no load. If the VOC concentration withinthe air inlet A is too high, the fuel mixture within the combustor 16will become too lean, thereby causing the combustor to "flame out.""Flame out" occurs when the fuel to air mixture within the combustorprimary-zone P becomes too lean to sustain a flame. In accordance withthis aspect of the present invention, air control system 110 is providedfor the purpose of enabling enrichment of the fuel burned withincombustor 16. As will be discussed in greater detail below, controlsystem 150 monitors and controls the concentration of the VOC within thesecondary fuel, as well as the overall fuel to air ratio within thecombustor, by causing a portion of the compressed air B to be directedonly within reaction chamber 18 and not into combustor 16.

Preferably, flow channels 112, 114 of system 110 each compriserespective tubes 116 and 118. Preferably, tubes 116 and 118 are suitablyattached to reaction chamber 18 at 116A, 118A and are in fluidcommunication with chamber 64 at inlets 124 and 126. Tubes 116 and 118each preferably include respective valves 120 and 122, which maycomprise any conventional flow control valve, such as a generalpoppet-type valve or the like. Tubes 116, 118 are in fluid communicationwith duct 65, which is in fluid communication with chamber 64, such thatwhen valves 120, 122 are opened, the pressure with chamber 64 pushes aportion of the compressed air B out of chamber 64 through duct 65 andinto tubes 116, 118. This portion of compressed air B then travelsthrough the tubes 116, 118 and exits through outlets 124, 126 causingair B to thereby bypass the combustor 16. In a preferred embodiment,when the valves 120, 122 are closed, all of compressed air B enterscombustor 16 in the region of openings 67A and 67B via inlets 69.

Preferably, as shown, channels 112 and 114, as well as duct 65, comprisea single tube that allow for the adequate bypass of compressed air Bfrom chamber 64 directly into reaction chamber 18. However, otherarrangements for accomplishing this objective easily can be devised andemployed in the context of the present invention. Due to sizeconsiderations, generally the number of channels 112, 114 are minimizedto two or three, and preferably even one; however, additional channelsmay be employed as desired.

Inlet air control system 110 can be activated manually or through thecomputer control associated with control system 150, which will now bedescribed.

Preferably, control system 150 is a computer based system suitablyconfigured and arranged to control, among other things, power generator12 and fuel supply C, as well as inlet and outlet air from device 10. Ingeneral, control system 150 operates in a conventional manner to controlpower generator 12 including, among other things, compressor 24 andturbine 26. Further, in a conventional fashion, control system 150operates to start device 10 initially and monitor operation of device 10as device 10 begins to operate due to the burning of primary fuel A andsecondary fuel C.

Control system 150, however, differs from conventional gas turbine andother industrial engine controls in that system 150 operates to monitorand, as necessary, adjust fuel supplies A and C, as well as air controlsystem 110 to achieve optimum levels of efficiency and ensure thatdevice 10 safely and effectively remains operative. As previously noted,and with momentary reference to FIG. 1, control system communicates andutilizes information received from sensors 42, 48, 52, and 72. Inaddition, one or more sensors 152 may be utilized which are incorporatedin proximity to or within reaction chamber 18 or combustor 16. (Whilesensor 152 is shown in FIG. 1 as being outside of both chamber 18 andcombustor 16, its location is only illustrative of its position (or thepositions) somewhere within fuel control system 14). In cooperation,these sensors provide information reflective of, among other things: VOClevel in inlet air (e.g. sensor 48); temperature and flow rate of inletair A, compressed air B, fuel C, mixed stream D and the like; fuelcontent and volume (e.g. sensor 74); power output from device 10; andspeeds of turbine 26. With this and other information, control systemsuitably controls the operation of device 10.

For example, when the power output of power generator 12 drops below anexpected level for the measured full consumption of fuel C, thusindicating, for example, that the fuel mixture within combustor 16 maybe becoming too lean, control system 150 may activate control system110. In such cases, valves 120, 122 will be opened thereby creating apressure difference sufficient to draw compressed air B out of thechamber 64 and into the bypass flow channels 112, 114, which in turn,direct compressed air B into reaction chamber 18 thus preventing itsflow into combustor 16. Operation of control system 150 in this mannerprevents the fuel mixture within combustor 16 from becoming too lean,while still allowing for the VOC laden air to be reacted with theprimary fuel within reaction chamber 18 to thereby destroy the VOCconcentration and retain the VOC fuel value.

Stated another way, control system 150, by monitoring the varying VOClevel in inlet air A, and thus the corresponding fuel valve of inletair, adjusts device 10 for appropriate operation. For example, in thecase where inlet air A has a fuel valve in excess of that necessary todrive power generator 12 at idle alone, control system 150 suitablyreduces the flow of fuel C and as necessary, activates air controlsystem 110 to prevent generator 12 from operating at excessive speedsand/or combustor from operating at excessively lean or such levels.

Control system 150 may also be employed to compensate for the relativelylong lag time between fuel introduction and changes in conditions atinlet 90 to turbine 26 caused by reactions taking place within reactionchamber 18, as well as to monitor or control other aspects of device 10.Control system 150 may employ any number of control processes andperform various computations known to those skilled in the art.

In accordance with a further embodiment of the present invention, andwith reference to FIG. 6, in some cases, it may be desirable toinitially treat VOC laden air from a typical plant prior to destroyingthe VOC's contained therein. In accordance with this aspect of thepresent invention, an air treatment system 200 is advantageouslyemployed and communicates with one or more destruction devices, forexample respective destruction devices 10A and 10B. Destruction devices10A and 10B are in a form similar to device 10 described above. System200 suitably comprises an inlet 202 which cooperates with, for example,inlet air duct 40. Inlet air A is thereafter drawn into chamber 203where inlet air A is both cooled and sampled to determine the level ofVOCs in inlet air A. Preferably, one or more sensors 206 are suitablycarried within chamber 203 for the purpose of determining the VOC levelwithin inlet air A.

In the event inlet air A is determined to be laden with an unacceptablelevel of VOC, an inlet bypass device 208 opens to allow fresh air intochamber 203. Preferably, bypass device 208 comprises a shutter valve ofconventional design.

In addition, inlet air A is suitably cooled to a temperature within anacceptable range. Preferably, such cooling is effected through a heatexchanger system 205. Preferably system 205 comprises respective heatexchange elements 204, 218, outlet 210 and cooling fan 222. As will beappreciated by those skilled in the art, element 204 is suitablyconnected via outlet and duct elements (not shown) to cooling pump 211and heat exchange element 218 such that cooling fluid is suitablyrecirculated between elements 204 and 218. In a conventional manner,system 205 allows for the cooling of inlet air A. Inlet air A oncecooled, is passed through a centrifugal separator 212 separating the VOCladen air from any large particles. Once separated, the VOC laden air iscommunicated to devices 10A and 10B, preferably by respective conduits214 and 216. As previously briefly mentioned, devices 10A and 10Boperate in a fashion similar to that of device 10 described above togenerate respective exhausts E1, E2 which are released into the plant toprovide process heat through respective outlet 230, 232.

With reference to FIG. 7, a further alternative embodiment of thepresent invention is shown. With certain applications, it may bedesirable to utilize a destruction device in accordance with the presentinvention in a relatively mobile fashion. As shown in FIG. 7, a mobiledestruction system 300 suitably comprises a sled 302 upon which adestruction device 10C is suitably mounted. Destruction device 10C issuitably configured in a manner similar to that of device 10 describedhereinabove. As so configured, device 10C includes power generator 12 towhich reaction chamber 18 and combustor 16 are suitably attached. Theoutput of device 10C, namely exhaust E3 is suitably communicated viaoutlet 303 into a heat recovery air-oil cooler 304. In accordance withthis embodiment of the present invention, a voltage source 306 issuitably provided to provide startup power to device 10C, as well aspower, at least initially, to the other aspects of system 300. A gascompressor 308 is also suitably mounted to sled 302 for raising gaspressure to levels required by device 10C. Respective ventilators 310,312 may be also suitably mounted to sled 302. In addition, a watersupply 320 with respective auxiliary units 322, 324, 326, 328 and pump330 may also be utilized for purposes of water injection into thecombustor 16 to control emissions of nitrous oxide.

System 300 is suitably controlled through operation of a control system350 which may be optionally cooled through operation of a refrigerationdevice 352. Various other devices such as ventilators, switch and otherelectronic devices may be also employed, in a conventional fashion, fora effective use of device 10C in connection with mobile system 300.

Preliminary experimental tests of devices embodying the presentinvention have indicated that by using the VOC laden secondary fuel, theamount of primary fuel needed to operate the engine is reduced without aloss of energy content in the fuel supply. Accordingly, the use of thisvolatile organic compound destruction system 10 results in substantiallycomplete destruction of the volatile organic compound while reducing theamount of primary fuel required to operate an engine for the generationof electricity.

Thus, it will be appreciated that device 10 provides significantadvantages over prior art designs for destruction of VOCs. For example,in accordance with experiments preformed using devices embodyingpreferred aspects of the present invention, substantial destruction ofVOC laden air efficiency (e.g. at rates above 99.5%) at a level of about6200 ft³ /min can be obtained with the production of a nominal 525 kw ofelectrical power.

To illustrate the overall impact of the present invention, consider atypical plant using 640,000 kw hours per month with a need to consume12,000 cubic feet per minute of air laden with 3,500 parts per millionof a VOC. Consider further that the plant consumes 97,000 therms offossil fuel each month. Without control, over 800 metric tons per yearof VOC's are released into the atmosphere.

While prior art techniques (e.g. use of a thermal oxidizer) may reducethe emission to less than 50 metric tons per year of VOC's, use of suchdevices increases the plant energy consumption to about 125,000 thermsper month.

In contradistinction, through use of a device embodying the presentinvention, effective VOC control is enabled with less energy.Specifically, in this example, the energy consumed and therefore, totalfossil fuels burned, falls to 81,000 therms per month. Not only are thetotal operating costs for the plant reduced, but there is also a netreduction in the emission of carbon dioxide, nitric oxide and sulfuroxide. The sum effect of use of the present invention to controlvolatile organic emissions is thus cleaner air, less fossil fuelconsumption and resulting lower costs.

It will be understood that the foregoing description is of the preferredexemplary embodiments of the invention, and that the invention is notlimited to the specific forms shown. Various modifications may be madein the design and arrangement of the elements set forth herein withoutdeparting from the scope of the invention as expressed in the appendedclaims.

We claim:
 1. A system for the destruction of volatile organic compounds(VOCs) comprising:a reaction chamber, said reaction chamber having acentral axis; a combustor attached to said reaction chambersubstantially perpendicular to sail central axis; an engine connected tosaid reaction chamber; wherein said system is configured to receive aprimary fuel and a secondary fuel, said secondary fuel comprising VOCladen air, and wherein said primary fuel is combusted in said combustorand said secondary fuel is combusted in said combustor and said reactionchamber.
 2. The system of claim 1 further comprising a compressor. 3.The system of claim 2 wherein said system further comprises an air inletduct, said inlet duct operatively connected to said compressor andenabling the communication to said compressor of said secondary fuel. 4.The system of claim 3, wherein said compressor is operatively connectedto said combustor and said reaction chamber.
 5. The system of claim 4wherein said reaction chamber defines a passageway, said passagewaycommunicating with a compressor outlet and an interior of said reactionchamber.
 6. The system of claim 5 further comprising a bypass systemoperatively connected to said passageway, said bypass system configuredto at least partially prevent flow of compressed secondary fuel to saidcombustor when said system is activated.
 7. The system of claim 6further comprising means for activating said bypass system.
 8. Thesystem of claim 7 wherein said activation means comprises means formonitoring VOC levels in said secondary fuel, means for monitoring theflow of said primary fuel and means for monitoring performance of saidengine.
 9. A system for the destruction of volatile organic compounds(VOCs) and the co-generation of power comprising:a power generatorincluding a compressor and a turbine; a reaction chamber having a firstsection, a second section, and an interior, said first sectioncommunicating with an outlet of said compressor and said second sectioncommunicating with an inlet to said turbine; a combustor attached tosaid reaction chamber, said combustor having an inlet configured toreceive a primary fuel supply and an outlet configured to directcombustion gases from said combustor into said reaction chamber in amanner effective to achieve a substantially cyclonic flow pattern ofsaid combustion gasses; and an air inlet connected to said compressorsuch that operation of said compressor draws in air laden with at leastone VOC; wherein said compressor, in operation, compresses said inletair to produce an amount of compressed inlet air; said first section ofsaid reaction chamber communicates with said interior of said reactionchamber and with said combustor such that a first portion of saidcompressed inlet air is directed by said first section of said combustorand a second portion of said compressed inlet air is directed by saidfirst section to said reaction chamber; and said combustor and saidreaction chamber are configured to destroy said at least one VOC and todirect said combustion gasses from said reaction chamber into saidturbine inlet to drive said turbine.
 10. The system of claim 9, whereinsaid power generator comprises a gas turbine engine.
 11. The system ofclaim 10, wherein said air inlet includes an air inlet sensor configuredto measure the amount of said at least one VOC in said inlet air; saidprimary fuel supply is provided by a primary fuel system, said primaryfuel system including a flow sensor configured to measure the flow ofsaid primary fuel supply directed to said combustor; said powergenerator includes a speed sensor configured to measure the speed ofsaid turbine; and said inlet sensor, said flow sensor, and said speedsensor provide information for controlling the operation of said system.12. The system of claim 11 further comprising a bypass system includingat least one duct means attached to said first section of said reactionchamber for preventing said compressed inlet air from being directedinto said combustor.
 13. The system of claim 12, further comprising acomputer control system configured to receive said sensor measurementsand initiate operation of said bypass system.